Notes from Mrs. Caso
These three projects were originally designed in 1998 for a symposium at NASA Glenn Research Center. They can still be found posted on their web site at http://www.grc.nasa.gov/WWW/K-12/problems/foilindex.html.
FoilSim is an interactive simulation software package that examines the airflow around various shapes of airfoils. As you change parameters such as airspeed, altitude, angle of attack, thickness and curvature of the airfoil, and size of the wing area, the software calculates the lift. The package was created at the NASA Glenn Research Center.
For more information on the program applet itself, see the links to the right.
Lesson Plan
Part 1: Wing Area Investigation (2 Days) | |
Objective(s): |
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Assessment: | You, or you and your partner, will be evaluated on the accuracy of your answers and creativity in design. |
Evaluation: | You will demonstrate the ability to use information found on the World Wide Web and in FoilSim to complete calculations involving area and lift and to design a unique wing planform. |
Part 2: Velocity Effects (2 Days) | |
Objective(s): |
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Assessment: | You, or you and your partner, will be evaluated on the accuracy of your answers and your ability to explain how you arrived at your decisions. |
Evaluation: | You will demonstrate the ability to use information found on the Internet and in FoilSim to complete the activities and discuss your findings. |
Part 3: Lift Equation Problems (1 Day) | |
Objective(s): |
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Assessment: | You, or you and your partner, will be evaluated on the accuracy of your answers and your ability to explain how you arrived at your decisions. |
Evaluation: | You will demonstrate the ability to use information found on the Internet and in FoilSim to complete the activities and discuss your findings. |